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PRINTER
HIGH GAIN
ANTENNA
AMPLIFIER
RADIO
FREQUENCY
UNIT
SATELLITE DATA
IRS UNIT
COMMUNICATIONS
CONTROL MANAGEMENT
SWITCHES SYSTEM
DATA LINK
PRINTER
CABIN DATA
PHONE HANDSET
FAX
PC/MODEM
TRANSMIT
RECEIVE
GROUND SYSTEM AIRBORNE SYSTEM
GROUND
STATION
UHF
MAGNASTAR
C−2000
COMMUNICATIONS
Rev 12, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
06−10−37
CABIN COMMUNICATION SYSTEM
The Cabin Communication System (CCS) provides a private automatic branch exchange switching
network. This network routes voice and data communications to and from up to nine active devices
(handsets/FAXs/modems/data link etc.) in the airplane and provides six air-to-ground channels. The
systems includes connections of basic telephone/telecomputing equipment to UHF antenna and
SATCOM links. In the event a data link device is installed on the airplane, the CCS has the capability
to communicate with the data link device using an internal modem.
The digital radio components consist of: one UHF antenna, duplexer and one airborne radio
telecommunication unit. The CCS plus all customer supplied handsets/FAXs/Modems is known as
the Office-In-The-Sky (OITS). The system will interface with personal computers, cabin handsets and
facsimile machines.
GF0610_069
The digital handset is located in the flight compartment and has a backlit LCD display and telephone
style keypad used to dial calls and select various options. A credit card reader (for optional billing) is
built into the handset and a two-button increase/decrease volume control (side of handset) is also
installed.
Refer to the Magnastar C-2000, G5000 ICG Aerocom A3000B and ICS-100 telephone system user
guide for description/function and operation of the system.
COMMUNICATIONS
Flight Crew Operating Manual Rev 12, Aug 14, 2006
CSP 700−5000−6
Volume 2
06−10−38
FLIGHT COMPARTMENT PRINTER
The flight compartment printer is installed in the copilot’s side console. The printer has ARINC 429
and laser quality thermal printer/plotter that is capable of full format and graphic printing from CAIMS
and DATALINK.
GF0610_070
FAULT
LOW
PPR
OPEN
PUSH PUSH TO CLOSE
OPEN
PUSH
The printer can be used to print selected messages and weather data sent to it via the Airborne Data
Link System (ADLS). The printer is also used by the Central Aircraft Information Maintenance
System (CAIMS) to print out certain maintenance fault and status information. This is accomplished
via the Portable Maintenance Access Terminal (PMAT).
GF0610_071
fault reporting can be printed by pressing
the button and a short report will be
printed even if no faults are detected.
PRINT MAINT REPORT Button − active
PRINT MAINT
REPORT
The PMAT can be used to generate an active fault report to the printer by operating the “PRINT
MAINT REPORT” button located on the left forward bulkhead in the flight compartment.
COMMUNICATIONS
Rev 12, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
06−10−39
FLIGHT COMPARTMENT PRINTER (CONT'D)
The printer interfaces with a communication link to the Airborne Data Link System (ADLS) and a
parallel interface from the PMAT.
GF0610_072
PMAT
AIRBORNE DATA LINK SYSTEM
PRINT MAINT PRINTER
REPORT
The printer push-buttons provide the following functions:
GF0610_073
or on when pressed.
door opened, illuminates in
conjunction with the TEST
indicator.
aural/visual alert function.
will illuminate all indicators
followed by a print out of test
results and pattern.
when the printer senses the
last remaining 10 feet of
paper on the supply roll.
advances paper while the
push−button is depressed.
OFF − turns the printer off
FAULT − paper out, printer
ALRT/RST − resets the printer
TEST − during the self−test,
LOW/PPR − illuminates
PPR PPR/ADV − continuously
ADV
LOW
PPR
TEST
ALRT
RST
FAULT
OFF
FAULT
LOW
PPR
OPEN
PUSH PUSH TO CLOSE
OPEN
PUSH
COMMUNICATIONS
Flight Crew Operating Manual Rev 12, Aug 14, 2006
CSP 700−5000−6
Volume 2
06−10−40
EICAS MESSAGES
FGF0610_001
SELCAL HF 1 (2)
Annunciated when HF1
or 2 indicates an
　
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